An aircraft propeller blade is constructed by forming two shells of composite material laminates and bonding the two shells to a metallic spar with foam filler pieces interposed between the shells at desired locations. The blade is then balanced radially and chordwise.
Method of making counterrotating aircraft propeller blades
1990-11-20
Sonstige
Keine Angabe
Englisch
Counterrotating aircraft propulsor blades
NTRS | 1988
|Counterrotating aircraft propulsor blades
NTRS | 1993
|The Acoustic Experimental Investigation of Counterrotating Propeller Configurations
SAE Technical Papers | 1987
|Performance and Acoustic Prediction of Counterrotating Propeller Configurations
SAE Technical Papers | 1989
|The acoustic experimental investigation of counterrotating propeller configurations
Tema Archiv | 1987
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